鼠笼式弹性支承结构参数优化设计与试验

冯国全; 周柏卓

鼠笼式弹性支承结构参数优化设计与试验

冯国全^1,2,
周柏卓³

1.
大连理工大学机械工程学院,大连 116024
2.
中国航空工业集团公司沈阳发动机设计研究所,沈阳 110015
3.
中国航空工业集团公司沈阳发动机设计研究所,沈阳 110015

计量
- 文章访问数: 1931
- HTML浏览量: 292
- PDF量: 37
- 被引次数: 0
出版历程
- 收稿日期: 2009-12-07
- 修回日期: 2010-09-01
- 刊出日期: 2011-01-28

Optimization design and test investigation of squirrel cage elastic support

FENG Guo-quan^1,2,
ZHOU Bai-zhuo³

1.
School of Mechanical Engineering, Dalian University of Technology,Dalian 116024,China
2.
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China,Shenyang 110015,China
3.
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China,Shenyang 110015,China

摘要

摘要: 进行了鼠笼式弹性支承的优化设计与试验研究.基于遗传算法和MATLAB开发了优化设计软件,进行了某航空发动机鼠笼式弹性支承的结构参数优化设计,并进行了柔度试验和疲劳应力试验.结果表明,疲劳应力下降到原来的40％,优化结果与试验结果的误差小于6%,验证了优化设计的有效性.
- 航空发动机 /
- 鼠笼式弹性支承 /
- 优化设计 /
- 支承柔度 /
- 整机振动 /
- 参数化设计
Abstract: Optimization design and test investigation of a squirrel cage elastic support was performed.An optimization software,which is used to achieve structure parameters optimization of squirrel cage elastic support of an engine,was developed based on the genetic algorithms and MATLAB.The test of flexibility and stress was accomplished.The results indicate that the fatigue stress is decreased to approximately 40% of the original scheme,the errors between the optimization and test results are less than 6%,so the optimization design is validated.
- aero-engine /
- squirrel cage elastic support /
- optimization design /
- support flexibility /
- engine vibration /
- parametric design

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参考文献(22)

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